As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) NR 1 ENGINE CONTINUOUS HIGH TEMPERATURE. STRIP INSPECTION FOUNDTHE FOLLOWING DEFECTS: HOLE BURNT IN INLET GUIDE VANE. FIRST STAGE NOZZLE BURNED AND PIECE MISSING . T5 HARNESS THERMOCOUPLE END BURNED OFF. POWER TURBINE VANE RING CRACKEDBETWEEN ADJACENT BLADES